[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 11th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16059 75 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 819 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
226/10:19:30
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 212
6
232/11:08:01
000 0
0 0
0 0
0
N/A 0
0 0
0 219
5
000/00:00:00
000 0
0 0
0 212
3
Coasting Arc #1 (Orbit 3649)
---------------------------------------
Vector Time (GMT): 2015/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6724266
31 A = 6786466
34 meter
Y = 851423
81 meter E =
0013786
Z = 157922
01 I = 51
70685
XDOT = -450
859636 Wp = 46
27083
YDOT = -4736
014188 meter/sec RA = 171
72955 deg
ZDOT = 6018
066462 TA = 315
42987
MA = 315
54065
Ha = 219
814 n
mi
Hp = 212
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22061241
19 X = -6734054
49
Y = 2793385
20 feet Y = 776173
91 meter
Z = 518116
81 Z = 125233
60
XDOT = -1479
198282 XDOT = -427
099919
YDOT = -15538
104292 feet/sec YDOT = -4740
923325 meter/sec
ZDOT = 19744
312541 ZDOT = 6015
933879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18223797
22 X = 5554613
39
Y = 12748363
73 feet Y = 3885701
26 meter
Z = 377154
55 Z = 114956
71
XDOT = -8315
178094 XDOT = -2534
466283
YDOT = 11260
231978 feet/sec YDOT = 3432
118707 meter/sec
ZDOT = 19735
905056 ZDOT = 6015
503861
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15222
56404314
00016717 00000-0 10270-3 0 9006
2 25544 51
6403 172
5356 0001462 39
2847 320
8412 15
55112936 36508
Satellite: ISS
Catalog Number: 25544
Epoch time: 15222
56404314 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 172
5356 deg
Eccentricity:
0001462
Arg of perigee: 39
2847 deg
Mean anomaly: 320
8412 deg
Mean motion: 15
55112936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3650
Checksum: 278
Coasting Arc #2 (Orbit 3664)
---------------------------------------
Vector Time (GMT): 2015/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6422491
11 A = 6784470
24 meter
Y = 247117
98 meter E =
0006276
Z = -2169893
21 I = 51
73287
XDOT = -2042
520287 Wp = 125
12537
YDOT = 4936
105385 meter/sec RA = 166
75850 deg
ZDOT = -5498
101039 TA = 78
91691
MA = 78
84634
Ha = 219
830 n
mi
Hp = 212
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21071165
07 X = 6429790
78
Y = 810754
54 feet Y = 318979
36 meter
Z = -7119072
21 Z = -2138676
85
XDOT = -6701
182045 XDOT = -2070
857997
YDOT = 16194
571474 feet/sec YDOT = 4913
106254 meter/sec
ZDOT = -18038
389234 ZDOT = -5508
091740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15353362
55 X = -4679704
90
Y = -14519708
79 feet Y = -4425607
24 meter
Z = -6984613
44 Z = -2128910
18
XDOT = 14563
318194 XDOT = 4438
899385
YDOT = -6724
866317 feet/sec YDOT = -2049
739254 meter/sec
ZDOT = -18082
247424 ZDOT = -5511
469015
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15223
52795786
00016717 00000-0 10270-3 0 9010
2 25544 51
6415 167
7228 0001508 38
8018 321
3243 15
55137435 36656
Satellite: ISS
Catalog Number: 25544
Epoch time: 15223
52795786 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 167
7228 deg
Eccentricity:
0001508
Arg of perigee: 38
8018 deg
Mean anomaly: 321
3243 deg
Mean motion: 15
55137435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3665
Checksum: 310
Coasting Arc #3 (Orbit 3680)
---------------------------------------
Vector Time (GMT): 2015/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5405700
38 A = 6780156
05 meter
Y = -1402871
60 meter E =
0012361
Z = 3834368
44 I = 51
74999
XDOT = 4229
347192 Wp = 92
46474
YDOT = -4856
197563 meter/sec RA = 161
77932 deg
ZDOT = 4173
700282 TA = 313
65110
MA = 313
75352
Ha = 219
852 n
mi
Hp = 212
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17735237
48 X = -5408236
90
Y = -4602597
12 feet Y = -1463335
91 meter
Z = 12579948
95 Z = 3808102
98
XDOT = 13875
810998 XDOT = 4263
062188
YDOT = -15932
406702 feet/sec YDOT = -4808
713747 meter/sec
ZDOT = 13693
242394 ZDOT = 4194
327045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10632136
12 X = 3240675
09
Y = 15016968
49 feet Y = 4577172
00 meter
Z = 12466996
55 Z = 3799940
55
XDOT = -19720
263111 XDOT = -6010
736196
YDOT = 2486
305924 feet/sec YDOT = 757
826045 meter/sec
ZDOT = 13782
925153 ZDOT = 4201
035587
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15224
55611496
00016717 00000-0 10270-3 0 9020
2 25544 51
6419 162
5898 0001402 44
1330 315
9935 15
55173856 36818
Satellite: ISS
Catalog Number: 25544
Epoch time: 15224
55611496 = yrday
fracday
Element set: 902
Inclination: 51
6419 deg
RA of node: 162
5898 deg
Eccentricity:
0001402
Arg of perigee: 44
1330 deg
Mean anomaly: 315
9935 deg
Mean motion: 15
55173856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3681
Checksum: 312
Coasting Arc #4 (Orbit 3695)
---------------------------------------
Vector Time (GMT): 2015/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3820556
79 A = 6775903
47 meter
Y = 2614046
00 meter E =
0013614
Z = -4960639
74 I = 51
76659
XDOT = -5868
477751 Wp = 71
09731
YDOT = 4403
019637 meter/sec RA = 156
78648 deg
ZDOT = -2200
180239 TA = 177
45577
MA = 177
44884
Ha = 219
742 n
mi
Hp = 212
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12534635
14 X = 3815138
34
Y = 8576266
42 feet Y = 2656739
64 meter
Z = -16275064
78 Z = -4942093
81
XDOT = -19253
535929 XDOT = -5906
589808
YDOT = 14445
602484 feet/sec YDOT = 4337
181348 meter/sec
ZDOT = -7218
439105 ZDOT = -2228
780141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4365897
13 X = -1330725
45
Y = -14635222
36 feet Y = -4460815
78 meter
Z = -16195566
24 Z = -4936408
59
XDOT = 22946
288629 XDOT = 6994
028774
YDOT = 1277
715683 feet/sec YDOT = 389
447740 meter/sec
ZDOT = -7342
419441 ZDOT = -2237
969446
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15225
51999628
00016717 00000-0 10270-3 0 9034
2 25544 51
6425 157
7767 0001495 45
3652 314
7623 15
55197806 36966
Satellite: ISS
Catalog Number: 25544
Epoch time: 15225
51999628 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 157
7767 deg
Eccentricity:
0001495
Arg of perigee: 45
3652 deg
Mean anomaly: 314
7623 deg
Mean motion: 15
55197806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3696
Checksum: 344
Coasting Arc #5 (Orbit 3710)
---------------------------------------
Vector Time (GMT): 2015/226/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4696068
21 A = 6777174
81 meter
Y = -1617747
37 meter E =
0009168
Z = 4604619
57 I = 51
79764
XDOT = 4762
287988 Wp = 106
94259
YDOT = -5204
179615 meter/sec RA = 152
15661 deg
ZDOT = 3020
907150 TA = 312
95631
MA = 313
03316
Ha = 219
735 n
mi
Hp = 212
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15407047
95 X = -4699996
18
Y = -5307570
11 feet Y = -1670283
74 meter
Z = 15107019
58 Z = 4581797
98
XDOT = 15624
304422 XDOT = 4805
454324
YDOT = -17074
080102 feet/sec YDOT = -5150
683149 meter/sec
ZDOT = 9911
112698 ZDOT = 3044
145889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2185360
62 X = 666097
92
Y = 16239641
92 feet Y = 4949842
86 meter
Z = 15008920
57 Z = 4574718
99
XDOT = -21044
772701 XDOT = -6414
446719
YDOT = -6444
476495 feet/sec YDOT = -1964
276436 meter/sec
ZDOT = 10012
129173 ZDOT = 3051
696972
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15226
48385922
00016717 00000-0 10270-3 0 9048
2 25544 51
6420 152
9641 0001272 48
0826 312
0436 15
55248531 37118
Satellite: ISS
Catalog Number: 25544
Epoch time: 15226
48385922 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 152
9641 deg
Eccentricity:
0001272
Arg of perigee: 48
0826 deg
Mean anomaly: 312
0436 deg
Mean motion: 15
55248531 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3711
Checksum: 290
Coasting Arc #6 (Orbit 3725)
---------------------------------------
Vector Time (GMT): 2015/227/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3001189
55 A = 6774362
45 meter
Y = 3012161
93 meter E =
0015699
Z = -5287333
08 I = 51
81607
XDOT = -6043
411027 Wp = 81
13439
YDOT = 4638
091591 meter/sec RA = 147
15955 deg
ZDOT = -787
697951 TA = 181
34489
MA = 181
34912
Ha = 219
669 n
mi
Hp = 212
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9846422
41 X = 2992967
13
Y = 9882421
02 feet Y = 3045677
01 meter
Z = -17346893
32 Z = -5272774
28
XDOT = -19827
463999 XDOT = -6090
999866
YDOT = 15216
835927 feet/sec YDOT = 4570
244079 meter/sec
ZDOT = -2584
310863 ZDOT = -817
170846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4156506
36 X = 1266903
14
Y = -13397535
63 feet Y = -4083568
86 meter
Z = -17284631
36 Z = -5268355
64
XDOT = 21675
955840 XDOT = 6606
831340
YDOT = 10225
375717 feet/sec YDOT = 3116
694518 meter/sec
ZDOT = -2712
117165 ZDOT = -826
653312
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15227
44770839
00016717 00000-0 10270-3 0 9051
2 25544 51
6422 148
1506 0001392 49
2724 310
8550 15
55235636 37261
Satellite: ISS
Catalog Number: 25544
Epoch time: 15227
44770839 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 148
1506 deg
Eccentricity:
0001392
Arg of perigee: 49
2724 deg
Mean anomaly: 310
8550 deg
Mean motion: 15
55235636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3726
Checksum: 306
Coasting Arc #7 (Orbit 3741)
---------------------------------------
Vector Time (GMT): 2015/228/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1080647
46 A = 6774802
02 meter
Y = -4274413
24 meter E =
0006167
Z = 5140387
45 I = 51
84467
XDOT = 6608
646233 Wp = 54
54499
YDOT = -3568
347194 meter/sec RA = 142
16160 deg
ZDOT = -1573
076112 TA = 50
59419
MA = 50
53961
Ha = 219
670 n
mi
Hp = 212
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3545431
29 X = -1057739
25
Y = -14023665
47 feet Y = -4286369
38 meter
Z = 16864788
22 Z = 5135193
84
XDOT = 21681
910212 XDOT = 6655
698463
YDOT = -11707
175834 feet/sec YDOT = -3494
181970 meter/sec
ZDOT = -5161
010866 ZDOT = -1540
858693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10574704
18 X = -3223169
84
Y = 9906557
91 feet Y = 3019518
85 meter
Z = 16843102
44 Z = 5133777
62
XDOT = -19934
707745 XDOT = -6076
098921
YDOT = -12714
702342 feet/sec YDOT = -3875
441274 meter/sec
ZDOT = -5021
537053 ZDOT = -1530
564494
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15228
47579445
00016717 00000-0 10270-3 0 9066
2 25544 51
6426 143
0176 0001395 52
0433 308
0846 15
55269452 37422
Satellite: ISS
Catalog Number: 25544
Epoch time: 15228
47579445 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 143
0176 deg
Eccentricity:
0001395
Arg of perigee: 52
0433 deg
Mean anomaly: 308
0846 deg
Mean motion: 15
55269452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3742
Checksum: 312
Coasting Arc #8 (Orbit 3756)
---------------------------------------
Vector Time (GMT): 2015/229/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -794915
16 A = 6778368
57 meter
Y = 5251662
75 meter E =
0008868
Z = -4220007
92 I = 51
88129
XDOT = -6411
420643 Wp = 103
02221
YDOT = 1992
788229 meter/sec RA = 137
17145 deg
ZDOT = 3692
240649 TA = 204
72697
MA = 204
76951
Ha = 219
579 n
mi
Hp = 212
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2607989
36 X = -833082
53
Y = 17229864
67 feet Y = 5242559
81 meter
Z = -13845170
35 Z = -4223962
45
XDOT = -21034
844628 XDOT = -6451
163228
YDOT = 6538
019123 feet/sec YDOT = 1920
869530 meter/sec
ZDOT = 12113
650422 ZDOT = 3660
999022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16234039
46 X = 4948135
23
Y = -6295186
50 feet Y = -1918772
85 meter
Z = -13863086
84 Z = -4225468
87
XDOT = 15632
274911 XDOT = 4764
717393
YDOT = 13966
524834 feet/sec YDOT = 4256
996769 meter/sec
ZDOT = 11978
631384 ZDOT = 3651
086846
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15229
43960742
00016717 00000-0 10270-3 0 9078
2 25544 51
6424 138
2041 0001352 53
4036 306
7242 15
55295163 37573
Satellite: ISS
Catalog Number: 25544
Epoch time: 15229
43960742 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 138
2041 deg
Eccentricity:
0001352
Arg of perigee: 53
4036 deg
Mean anomaly: 306
7242 deg
Mean motion: 15
55295163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3757
Checksum: 295
Coasting Arc #9 (Orbit 3772)
---------------------------------------
Vector Time (GMT): 2015/230/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2457682
62 A = 6782922
56 meter
Y = -5752075
62 meter E =
0014576
Z = 2607278
77 I = 51
91990
XDOT = 5580
728925 Wp = 99
23200
YDOT = -12
644017 meter/sec RA = 132
19787 deg
ZDOT = -5265
690983 TA = 51
50796
MA = 51
37732
Ha = 219
532 n
mi
Hp = 212
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8063263
18 X = 2509156
02
Y = -18871639
18 feet Y = -5724304
22 meter
Z = 8554064
19 Z = 2619342
99
XDOT = 18309
478102 XDOT = 5606
034001
YDOT = -41
482996 feet/sec YDOT = 49
904492 meter/sec
ZDOT = -17275
889052 ZDOT = -5238
519739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20324270
77 X = -6194837
73
Y = 2677677
76 feet Y = 816156
18 meter
Z = 8607035
02 Z = 2623424
27
XDOT = -9190
623158 XDOT = -2801
301939
YDOT = -14366
526226 feet/sec YDOT = -4378
917194 meter/sec
ZDOT = -17158
737819 ZDOT = -5229
983287
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15230
46765644
00016717 00000-0 10270-3 0 9088
2 25544 51
6428 133
0700 0001359 56
6253 303
5030 15
55328621 37739
Satellite: ISS
Catalog Number: 25544
Epoch time: 15230
46765644 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 133
0700 deg
Eccentricity:
0001359
Arg of perigee: 56
6253 deg
Mean anomaly: 303
5030 deg
Mean motion: 15
55328621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3773
Checksum: 291
Coasting Arc #10 (Orbit 3787)
---------------------------------------
Vector Time (GMT): 2015/231/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3695560
54 A = 6785630
82 meter
Y = 5651774
76 meter E =
0011994
Z = -610631
11 I = 51
94930
XDOT = -4266
167584 Wp = 42
65451
YDOT = -2149
521013 meter/sec RA = 127
23840 deg
ZDOT = 6001
120538 TA = 310
77842
MA = 310
88243
Ha = 219
505 n
mi
Hp = 212
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12124542
44 X = -3755519
19
Y = 18542568
12 feet Y = 5610113
29 meter
Z = -2003382
91 Z = -628729
29
XDOT = -13996
612809 XDOT = -4270
964999
YDOT = -7052
234294 feet/sec YDOT = -2197
254521 meter/sec
ZDOT = 19688
715676 ZDOT = 5980
384996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22138078
33 X = 6747686
28
Y = 643545
74 feet Y = 196152
74 meter
Z = -2082364
45 Z = -634704
69
XDOT = 1410
451693 XDOT = 429
905676
YDOT = 14110
757259 feet/sec YDOT = 4300
958813 meter/sec
ZDOT = 19599
668537 ZDOT = 5973
978970
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15231
43143502
00016717 00000-0 10270-3 0 9090
2 25544 51
6423 128
2565 0001327 56
7571 303
3710 15
55341945 37881
Satellite: ISS
Catalog Number: 25544
Epoch time: 15231
43143502 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 128
2565 deg
Eccentricity:
0001327
Arg of perigee: 56
7571 deg
Mean anomaly: 303
3710 deg
Mean motion: 15
55341945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3788
Checksum: 295
Coasting Arc #11 (Orbit 3803)
---------------------------------------
Vector Time (GMT): 2015/232/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4482839
79 A = 6784756
73 meter
Y = -4853514
43 meter E =
0008593
Z = -1530896
82 I = 51
96596
XDOT = 2656
685413 Wp = 134
35555
YDOT = 4271
150381 meter/sec RA = 122
28372 deg
ZDOT = -5787
552066 TA = 62
29812
MA = 62
21096
Ha = 219
491 n
mi
Hp = 212
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14707479
64 X = 4544216
27
Y = -15923603
78 feet Y = -4803041
29 meter
Z = -5022627
37 Z = -1508970
81
XDOT = 8716
159491 XDOT = 2636
840520
YDOT = 14012
960569 feet/sec YDOT = 4300
747863 meter/sec
ZDOT = -18988
031711 ZDOT = -5774
694950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21347708
56 X = -6506781
57
Y = -3885271
31 feet Y = -1184230
70 meter
Z = -4927261
56 Z = -1501829
32
XDOT = 6792
715254 XDOT = 2070
419610
YDOT = -13421
259483 feet/sec YDOT = -4090
799890 meter/sec
ZDOT = -18933
312979 ZDOT = -5770
873796
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15232
45944740
00016717 00000-0 10270-3 0 9108
2 25544 51
6432 123
1217 0001258 62
5429 297
5852 15
55371532 38044
Satellite: ISS
Catalog Number: 25544
Epoch time: 15232
45944740 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 123
1217 deg
Eccentricity:
0001258
Arg of perigee: 62
5429 deg
Mean anomaly: 297
5852 deg
Mean motion: 15
55371532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3804
Checksum: 296
Coasting Arc #12 (Orbit 3804)
---------------------------------------
Vector Time (GMT): 2015/232/11:08:01
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4766669
14 A = 6783583
87 meter
Y = 4245482
57 meter E =
0015199
Z = 2274660
17 I = 51
96261
XDOT = -1877
726794 Wp = 70
97138
YDOT = -5049
414748 meter/sec RA = 122
12201 deg
ZDOT = 5464
619639 TA = 314
25494
MA = 314
37959
Ha = 219
542 n
mi
Hp = 212
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15638678
29 X = -4824838
27
Y = 13928748
60 feet Y = 4191853
45 meter
Z = 7462795
85 Z = 2251363
21
XDOT = -6160
520979 XDOT = -1847
668381
YDOT = -16566
321351 feet/sec YDOT = -5070
244316 meter/sec
ZDOT = 17928
542124 ZDOT = 5455
571385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20932891
90 X = 6380345
45
Y = 1375570
69 feet Y = 419273
95 meter
Z = 7361620
75 Z = 2243822
00
XDOT = -7278
603961 XDOT = -2218
518487
YDOT = 14576
767659 feet/sec YDOT = 4442
998783 meter/sec
ZDOT = 17890
379039 ZDOT = 5452
987531
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15232
52369788
00016717 00000-0 10270-3 0 9110
2 25544 51
6432 122
8009 0001348 60
9009 299
2279 15
55371630 38057
Satellite: ISS
Catalog Number: 25544
Epoch time: 15232
52369788 = yrday
fracday
Element set: 911
Inclination: 51
6432 deg
RA of node: 122
8009 deg
Eccentricity:
0001348
Arg of perigee: 60
9009 deg
Mean anomaly: 299
2279 deg
Mean motion: 15
55371630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3805
Checksum: 311
Coasting Arc #13 (Orbit 3819)
---------------------------------------
Vector Time (GMT): 2015/233/11:08:01
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4837079
10 A = 6778897
79 meter
Y = -2570572
75 meter E =
0008006
Z = -4002019
11 I = 51
96422
XDOT = 165
786086 Wp = 71
23145
YDOT = 6533
361943 meter/sec RA = 117
15446 deg
ZDOT = -4000
143738 TA = 157
27203
MA = 157
23657
Ha = 219
394 n
mi
Hp = 212
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15869682
07 X = 4884904
58
Y = -8433637
65 feet Y = -2516214
16 meter
Z = -13129983
95 Z = -3978405
32
XDOT = 543
917604 XDOT = 112
147247
YDOT = 21434
914512 feet/sec YDOT = 6534
915748 meter/sec
ZDOT = -13123
831160 ZDOT = -3999
469013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17301417
38 X = -5273472
02
Y = -5129242
71 feet Y = -1563393
18 meter
Z = -13027714
97 Z = -3970847
52
XDOT = 14168
363170 XDOT = 4318
517094
YDOT = -14496
447076 feet/sec YDOT = -4418
517069 meter/sec
ZDOT = -13122
037109 ZDOT = -3999
596911
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15233
48744054
00016717 00000-0 10270-3 0 9120
2 25544 51
6439 117
9872 0001230 60
8649 299
2628 15
55417309 38205
Satellite: ISS
Catalog Number: 25544
Epoch time: 15233
48744054 = yrday
fracday
Element set: 912
Inclination: 51
6439 deg
RA of node: 117
9872 deg
Eccentricity:
0001230
Arg of perigee: 60
8649 deg
Mean anomaly: 299
2628 deg
Mean motion: 15
55417309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3820
Checksum: 319
Coasting Arc #14 (Orbit 3835)
---------------------------------------
Vector Time (GMT): 2015/234/11:08:01
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4472630
72 A = 6774741
13 meter
Y = 483752
14 meter E =
0006419
Z = 5061209
07 I = 51
96421
XDOT = 1369
332669 Wp = 114
98915
YDOT = -7306
920976 meter/sec RA = 112
17190 deg
ZDOT = 1903
963919 TA = 316
62467
MA = 316
67517
Ha = 219
506 n
mi
Hp = 212
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14673985
29 X = -4502293
09
Y = 1587113
33 feet Y = 433570
60 meter
Z = 16605016
64 Z = 5039409
93
XDOT = 4492
561251 XDOT = 1441
689949
YDOT = -23972
837849 feet/sec YDOT = -7291
203547 meter/sec
ZDOT = 6246
600783 ZDOT = 1910
791888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11830935
99 X = 3606069
29
Y = 8999430
68 feet Y = 2743026
47 meter
Z = 16510922
18 Z = 5032529
08
XDOT = -19048
482331 XDOT = -5805
977414
YDOT = 13497
603643 feet/sec YDOT = 4114
069590 meter/sec
ZDOT = 6277
308280 ZDOT = 1913
323564
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15234
51541639
00016717 00000-0 10270-3 0 9130
2 25544 51
6438 112
8522 0001228 65
9333 294
1949 15
55440333 38363
Satellite: ISS
Catalog Number: 25544
Epoch time: 15234
51541639 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node: 112
8522 deg
Eccentricity:
0001228
Arg of perigee: 65
9333 deg
Mean anomaly: 294
1949 deg
Mean motion: 15
55440333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3836
Checksum: 307
Coasting Arc #15 (Orbit 3850)
---------------------------------------
Vector Time (GMT): 2015/235/11:08:01
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3805603
53 A = 6773510
29 meter
Y = 1787736
18 meter E =
0015758
Z = -5324127
04 I = 51
97198
XDOT = -2642
277017 Wp = 91
88048
YDOT = 7170
098759 meter/sec RA = 107
18032 deg
ZDOT = 519
739537 TA = 183
05669
MA = 183
06633
Ha = 219
261 n
mi
Hp = 212
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12485575
89 X = 3811192
27
Y = 5865276
19 feet Y = 1830324
04 meter
Z = -17467608
41 Z = -5305626
74
XDOT = -8668
887852 XDOT = -2724
783101
YDOT = 23523
946060 feet/sec YDOT = 7140
089777 meter/sec
ZDOT = 1705
182209 ZDOT = 506
703337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5346337
19 X = -1629563
58
Y = -12824898
27 feet Y = -3909028
99 meter
Z = -17388130
33 Z = -5299902
13
XDOT = 21338
345534 XDOT = 6503
927719
YDOT = -11125
660979 feet/sec YDOT = -3391
101466 meter/sec
ZDOT = 1647
707424 ZDOT = 502
221223
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15235
47912693
00016717 00000-0 10270-3 0 9149
2 25544 51
6442 108
0381 0001152 62
9759 297
1512 15
55479141 38518
Satellite: ISS
Catalog Number: 25544
Epoch time: 15235
47912693 = yrday
fracday
Element set: 914
Inclination: 51
6442 deg
RA of node: 108
0381 deg
Eccentricity:
0001152
Arg of perigee: 62
9759 deg
Mean anomaly: 297
1512 deg
Mean motion: 15
55479141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3851
Checksum: 311
Coasting Arc #16 (Orbit 3866)
---------------------------------------
Vector Time (GMT): 2015/236/11:08:01
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2905014
30 A = 6775954
77 meter
Y = -3924140
80 meter E =
0009136
Z = 4693358
20 I = 51
98947
XDOT = 3620
587578 Wp = 63
24498
YDOT = -6125
910976 meter/sec RA = 102
19231 deg
ZDOT = -2872
596830 TA = 55
16448
MA = 55
07858
Ha = 219
232 n
mi
Hp = 212
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9530886
81 X = -2883716
10
Y = -12874477
68 feet Y = -3956507
40 meter
Z = 15398156
82 Z = 4679298
13
XDOT = 11878
568168 XDOT = 3702
773794
YDOT = -20098
133124 feet/sec YDOT = -6084
963713 meter/sec
ZDOT = -9424
530281 ZDOT = -2854
809115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1296755
02 X = -395250
93
Y = 16023455
58 feet Y = 4883949
26 meter
Z = 15338204
26 Z = 4675084
66
XDOT = -21081
280459 XDOT = -6425
574284
YDOT = 7267
100202 feet/sec YDOT = 2215
012142 meter/sec
ZDOT = -9346
728509 ZDOT = -2848
882849
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15236
50706690
00016717 00000-0 10270-3 0 9153
2 25544 51
6444 102
9033 0001086 58
3130 301
8129 15
55531921 38674
Satellite: ISS
Catalog Number: 25544
Epoch time: 15236
50706690 = yrday
fracday
Element set: 915
Inclination: 51
6444 deg
RA of node: 102
9033 deg
Eccentricity:
0001086
Arg of perigee: 58
3130 deg
Mean anomaly: 301
8129 deg
Mean motion: 15
55531921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3867
Checksum: 291
Coasting Arc #17 (Orbit 3881)
---------------------------------------
Vector Time (GMT): 2015/237/11:08:01
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1894692
03 A = 6780687
59 meter
Y = 5609092
60 meter E =
0005613
Z = -3309161
24 I = 52
01080
XDOT = -4273
081482 Wp = 80
24180
YDOT = 4238
882025 meter/sec RA = 97
21762 deg
ZDOT = 4746
146366 TA = 241
51076
MA = 241
56731
Ha = 219
168 n
mi
Hp = 212
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6216181
20 X = 1847903
47
Y = 18402534
79 feet Y = 5630018
62 meter
Z = -10856828
22 Z = -3300071
05
XDOT = -14019
296202 XDOT = -4343
218847
YDOT = 13907
093259 feet/sec YDOT = 4190
705548 meter/sec
ZDOT = 15571
346344 ZDOT = 4725
218361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7151662
18 X = 2179826
63
Y = -18082483
75 feet Y = -5511541
05 meter
Z = -10818614
70 Z = -3297513
76
XDOT = 18448
385600 XDOT = 5623
067931
YDOT = -1950
110328 feet/sec YDOT = -594
393628 meter/sec
ZDOT = 15480
319326 ZDOT = 4718
401330
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15237
47074608
00016717 00000-0 10270-3 0 9168
2 25544 51
6442 98
0891 0001022 59
2675 300
8579 15
55513472 38829
Satellite: ISS
Catalog Number: 25544
Epoch time: 15237
47074608 = yrday
fracday
Element set: 916
Inclination: 51
6442 deg
RA of node: 98
0891 deg
Eccentricity:
0001022
Arg of perigee: 59
2675 deg
Mean anomaly: 300
8579 deg
Mean motion: 15
55513472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3882
Checksum: 321
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